EP3615849B1 - Ölabstreifring-feder für einen ölabstreifring und ölabstreifring - Google Patents
Ölabstreifring-feder für einen ölabstreifring und ölabstreifring Download PDFInfo
- Publication number
- EP3615849B1 EP3615849B1 EP18719565.6A EP18719565A EP3615849B1 EP 3615849 B1 EP3615849 B1 EP 3615849B1 EP 18719565 A EP18719565 A EP 18719565A EP 3615849 B1 EP3615849 B1 EP 3615849B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- recess
- ring spring
- oil scraper
- scraper ring
- oil
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 239000002184 metal Substances 0.000 claims description 80
- 230000000875 corresponding effect Effects 0.000 claims 1
- 238000002485 combustion reaction Methods 0.000 description 9
- 230000002093 peripheral effect Effects 0.000 description 8
- 230000000284 resting effect Effects 0.000 description 7
- 239000000463 material Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000003344 environmental pollutant Substances 0.000 description 2
- 231100000719 pollutant Toxicity 0.000 description 2
- 125000006850 spacer group Chemical group 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/064—Rings with a flat annular side rail
- F16J9/066—Spring expander from sheet metal
- F16J9/068—Spring expander from sheet metal corrugated in the axial direction
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/064—Rings with a flat annular side rail
- F16J9/066—Spring expander from sheet metal
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J9/00—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction
- F16J9/06—Piston-rings, e.g. non-metallic piston-rings, seats therefor; Ring sealings of similar construction using separate springs or elastic elements expanding the rings; Springs therefor ; Expansion by wedging
- F16J9/064—Rings with a flat annular side rail
Definitions
- the invention relates to an oil control ring spring for an oil control ring, which has the oil control ring spring, an upper and a lower metal ring and is intended to be mounted in an oil ring groove of a piston.
- the invention also relates to a corresponding oil control ring.
- Oil control rings are used in internal combustion engines arranged in a groove of a piston (piston groove) of the internal combustion engine and have the task of scraping off excess oil from an inner wall of the cylinder or the inner wall of the cylinder liner during operation. It is known to design oil control rings in several parts, for example in three parts from an upper metal ring, a lower metal ring and an oil control ring spring arranged between them.
- the EP 2 703 695 B1 Fig. 12 shows an oil control ring spring having a plurality of upper portions and a plurality of lower portions arranged alternately in a circumferential direction so that they are spaced apart in an axial direction and spaced apart in the circumferential direction. Connection areas are provided which each connect the adjacent upper and lower areas to one another. Each of the upper and lower areas has a nose portion which is arranged at the inner peripheral end and is designed to press the respective adjacent upper or lower metal ring radially outward.
- the nose section has a through opening.
- a support section is provided on each of the upper and lower regions, which extends radially between the nose section and the outer circumferential end and is designed so that the respective upper or lower metal ring rests thereon or rests against it.
- a recess is formed which has a constant depth in the radial direction of the oil control ring spring.
- the oil flow is between the oil control ring spring and the upper or lower metal ring when the internal combustion engine is operating low, so that residues, for example combustion residues, collect there. Due to the relative movements between the oil control ring spring and the metal rings, these residues cause wear on both the metal rings and the oil control ring spring.
- the JP 2012 233572 A starts from the problem of preventing sticking between the side rails and a spacer of a combined oil ring, and proposes a combined oil ring with a pair of upper and lower side rails and a spacer-expander arranged therebetween.
- the spacer expander includes many upper and lower parts alternately arranged in the axial and circumferential directions, connectors for connecting the upper and lower parts, and nose portions raised from the inner peripheral side ends of the upper and lower parts for pressing the side rails and having holes .
- An oil control ring spring according to the invention for an oil control ring which has the oil control ring spring, an upper and a lower metal ring and is intended to be mounted in an oil ring groove of a piston, has the following: several upper areas and several lower areas, which alternate in are arranged in a circumferential direction so as to be spaced apart in an axial direction; Connecting portions each connecting the adjacent upper and lower portions with each other; each of the upper and lower regions each having: a nose portion which is arranged at the inner peripheral end and is configured to press the respective adjacent, upper or lower metal ring radially outward, and which has a through opening; a support portion which extends radially between the nose portion and the outer peripheral end and is designed so that the respective upper or lower metal ring rests thereon or rests thereon; wherein a recess is formed in the support section, the depth of which, based on the support surface of the support section, increases in the radial direction towards the through opening, and / or whose width increases in the radial direction
- the oil is stripped from the cylinder liner and directed inwards to the radial inner diameter of the oil control ring spring, where it is fed back into the system via the oil return bores provided on the piston.
- an oil pressure builds up on the radial outer diameter and on the inner diameter of the oil control ring spring, with part of the oil flowing back into the embossed depressions of the spring and there the upper or lower metal ring is pressed axially in the direction of the upper and lower piston groove flanks.
- the respective metal ring is able to better seal the piston groove axially against possible combustion gases.
- the metal ring pumps the oil out of the groove, whereby this can easily flow off to the inside diameter of the oil control ring spring due to the inclined position of the recess.
- the above-described oil pressure on the outer or inner diameter of the oil control ring spring can be further adapted or influenced by the depth or the angle of the recess, which can be between 5 ° and 30 ° depending on the requirements due to the engine running properties.
- the recess formed in the respective support section thus promotes the oil in the radial direction of the oil control ring spring when the oil control ring spring moves axially.
- the depth or width of the recess increases towards the passage opening, so that there is an oil flow through the passage opening.
- the oil control ring spring according to the invention generates an increased flow of oil between the oil control ring spring and the adjacent metal rings when the internal combustion engine is in operation. As a result, combustion residues from this area are removed together with the oil. Furthermore, aging of the oil caused by staying in this area for too long is avoided. As a result, the friction between the ring and the spring and the resulting secondary wear can be reduced and thus the pollutant emissions can be improved.
- the oil control ring spring according to the invention enables reduced oil carbon formation due to increased flow speed and thus no compression of the oil and the resulting oil carbon formation between the spring and the adjacent metal rings.
- axial sealing of the piston groove is improved by hydrostatically pressing the metal rings against the upper and lower piston groove flanks.
- the recess in the support section essentially has the shape of a half-funnel.
- the semi-funnel-shaped design of the recess in the support section enables the increase in depth to run uniformly in the direction of the through opening.
- the half-funnel preferably has an opening angle of 30 ° to 150 °, particularly preferably 30 ° to 60 °. In the narrower angular range, there is a particularly good delivery effect with regard to the oil in the radial direction. At the same time, the opening angle of the semi-funnel-shaped depression is so large that there is a sufficient delivery volume in the depression for the oil.
- the recess serves to enlarge and accelerate the oil flow towards the center of the piston.
- the depression is radial in its depth or width towards the inside, ie towards a piston enclosed by the oil control ring spring
- an accelerated oil flow of the oil delivered by the oil control ring spring and the associated metal rings is achieved in the radial direction, ie towards the center of the piston.
- the recess interacts with the adjoining passage opening and offers a good drainage point for the oil together with the combustion residues.
- the radially outer end of the recess is arranged in the support section at a recess start position which is spaced apart from the outer circumferential end, in particular by 20 to 30% of the width of the oil control ring spring, viewed in the radial direction, spaced apart from the outer circumferential end is.
- a region of the support section remains free of the depression, which results in a larger contact surface for the metal ring on the support section of the oil control ring spring.
- the load on the oil control ring spring by the metal ring in the area of the support section can be reduced.
- the abrasion of the oil control ring spring caused by the metal ring resting on the oil control ring spring is reduced.
- the part of the support section between the recess start position and the outer peripheral end lies in the radial plane of the support section.
- a radial plane is understood here to mean a plane which touches the support section and in particular intersects the axis of symmetry of the oil control ring spring at a right angle. This results in a partially flat contact of the metal ring on the oil control ring spring, as a result of which the surface load in the contact area between the oil control ring spring and the metal ring is kept low and wear is minimized. This is particularly advantageous in the case of small relative movements between the oil control ring spring and the metal ring resting on it.
- the radially inner end of the recess has a maximum depth of 0.05 mm in relation to the plane of the support section. Series of tests have shown that even at this shallow depth of the depression, the oil delivery effect in the direction of the passage opening occurs to an adequate extent. A small depth of the formed recess offers the advantage of large possible radii of curvature of the oil control ring spring in the area of the support section and thus low punctual or linear loads in the contact area with the metal ring.
- the radially outer end of the depression is arranged in the support section at a depression start position, the width of which corresponds in particular to the width of 10 to 20% of the width of the through opening.
- the width of the through opening is understood here to mean its maximum extent in the circumferential direction of the oil control ring spring.
- the width of the recess in the support section increases in the radial direction from the recess start position to the radial position of the through opening, in particular so that the width of the recess at the radial position of the through opening corresponds to the width of the through opening.
- the recess viewed in the circumferential direction of the oil control ring spring, where it opens into the through opening, is the same width as the through opening. This results in a particularly undisturbed drainage of the oil that collects in the depression during operation into the passage opening. A build-up of oil on the nose section is largely avoided.
- the width of the through opening is at least 0.1 to 0.7 mm. With this width, a good flow through the passage opening is achieved even with a high viscosity of the oil, for example 21.9 mm 2 / s.
- the cut surface of the through opening lies essentially in the axial direction and / or has an area of 0.1 to 0.5 square millimeters.
- the height of the through opening measured essentially in the axial direction from the bottom of the highest part of the Nose section to the top of the deepest part of the recess 0.1-0.9 mm.
- the direction of extension of the recess lies in the radial direction; and / or the recess is aligned with the respective through opening.
- the radial extension direction of the recess offers a particularly short transport path for the oil in the radial direction over the oil control ring spring.
- the depression is preferably in the radial direction, i. This means that it is symmetrical, perpendicular to the circumferential direction of the oil control ring spring. Because the recess is in alignment with the respective through opening, an optimal transport of the oil that has accumulated in the recess is achieved through the through opening. A build-up of oil at the passage opening is avoided.
- the top of the bottom of the recess forms an angle of 3-30 ° with the radial plane; and / or the upper side edges or side flanks of the recess span an angular segment of 5-50 °, preferably 5-15 °.
- the top of the base preferably encloses an angle of 3-30 ° with the radial plane when viewed in the radial direction.
- the upper side of the bottom of the recess is understood here to mean the area in which the oil collects, that is to say has a trough-shaped shape.
- the angle of 3-30 ° leads to good drainage behavior of the oil in the direction of the passage opening.
- the oil is pressed into the recess by the oscillating movement of the oil control ring spring together with the piston due to its inertia and viscosity.
- the resulting pressure together with the angle of 3-30 °, causes the oil to run off on the top of the base towards the passage opening.
- the angular range of 5-50 °, preferably of 5-15 °, for the angular segment of the side edges of the recess is measured in a plane that runs parallel to the axis of extension of the oil control ring spring and in particular orthogonally to the direction of extension of the recess. In the aforementioned angular range, there is very good channel-like collection of the oil in the depression.
- the radial width of the nose section is 0.2 to 1.2 mm; and / or the radial width of the support section is 0.1 to 1.1 mm.
- the radial width of the nose section is understood to mean its maximum extent in the circumferential direction of the oil control ring spring.
- the radial width of the support section is understood to mean its maximum extent in the circumferential direction of the oil control ring spring.
- the invention relates to an oil control ring to be mounted in an oil ring groove of a piston, having an oil control ring spring, an upper metal ring which rests on the support sections of the upper areas of the oil control ring spring and its radial inner surface on the radial outer surfaces of the nose sections the upper area of the oil control ring spring rests; and a lower metal ring which rests against the bearing portions of the lower regions of the oil control ring spring and the radially inner surface of which rests against the radially outer surface of the nose portions of the lower regions of the oil control ring spring.
- Fig. 1 shows an oil control ring spring 1 for an oil control ring 3 (in Fig. 1 not shown) according to an embodiment in plan view and two side views.
- the oil control ring spring 1 is shown in a top view.
- the oil control ring spring 1 lies essentially in a circular manner in the image plane of FIG Fig. 1 .
- the section plane AA runs through the vertical axis of symmetry of the oil control ring spring 1 orthogonally into the image plane.
- On the right in the picture there is a sectional view of the oil control ring spring 1 seen in the section plane AA.
- a side view of the oil control ring spring 1 is shown on the left in the picture.
- the letter E marks a detail in the sectional view which, with reference to FIG Fig. 4 is described.
- the letter F indicates a detail in the side view shown on the left that relates to FIG Fig. 3 is set out.
- FIG. 13 shows a partial area of the oil control ring spring 1 according to the exemplary embodiment from FIG Fig. 1 in a perspective view.
- the section shown represents a ring segment of the oil control ring spring 1.
- the in Fig. 2 The representation shown results, for example, from the middle representation of Fig. 1 by cutting out the lower part of the oil control ring spring 1 in the picture and swiveling it upwards over into the plane of the picture.
- the oil control ring spring 1 according to this exemplary embodiment is designed essentially symmetrically to a radial plane which is oriented perpendicular to the axis of symmetry of the oil control ring spring.
- a plurality of upper areas 5 and a plurality of lower areas 7 are arranged alternately in a circumferential direction of the oil control ring spring 1, so that they are spaced apart in the axial direction and in the circumferential direction, upper areas 5 arranged directly next to one another and lower areas 7 arranged directly next to one another are spaced apart from one another in the circumferential direction are.
- Connection areas 9 connect the respectively adjacent upper areas 5 and lower areas 7.
- the connection areas have rounded portions 11 so that the upper areas 5 and the lower areas 7 merge into one another in a rounded manner via the connection areas 9. This shape is good as an approximate wavy line on the side facing the viewer, which at the same time forms the outer circumference of the oil control ring spring 1, in Fig. 2 recognizable.
- Each of the upper areas 5 and lower areas 7 has a nose portion 13 located at the inner peripheral end.
- the nose sections 13 each have a through opening 15.
- the nose sections 13 can be seen at the rear edge of the picture as a rounded V turned upside down.
- the nose sections 13 of the upper areas 5 protruding upward in the picture can be seen, while the nose sections 13 of the lower areas 7 protruding downward are covered in the illustration.
- the lower nose portions 13 are in the FIGS. 3 and 4 good to see.
- Each of the upper areas 5 and the lower areas 7 furthermore has a bearing portion 17, which extends radially between the nose portion 13 and the outer peripheral end and is designed so that an upper metal ring 21 (in Fig. 2 not shown) or lower metal ring 23 (in Fig. 2 not shown) of the oil control ring 3 rests on it or rests against it.
- An oil control ring 3 then contains the oil control ring spring 1, an upper metal ring 21 resting on the support section 17 of the upper region 5, and a lower metal ring 23 resting on the support section of the lower region 7.
- the nose sections 13 are designed to limit the freedom of movement of the metal rings 21, 23 radially inward.
- the respective metal ring 21, 23 then runs past the nose sections 13 radially on the outside and rests directly on the nose sections 13, for example. In this way, the upper and lower metal rings 21, 23 are centered coaxially with the oil control ring spring 1.
- a recess 19 is formed in each support section 17, the depth of which, based on the support surface of the support section 17, increases in the radial direction towards the through opening 15 and the width increases in the radial direction towards the through opening 15.
- the depressions 19 can be seen in the image in a V-shape on the support sections of the upper areas.
- the depressions 19 begin approximately at two-thirds of the radial extent of the support section 17 from the outer circumference of the oil control ring spring 1. Towards the through opening 15, the depth and width of the depression 19 then increases.
- the depressions on the support sections 17 of the lower areas 7 can be seen as bulges upward in the image.
- the radially outer end of the recess 19 is arranged in the support section 17 at a recess start position 20, which is spaced from the outer peripheral end. This results in an enlarged, recess-free contact surface for the respective metal ring 21, 23.
- the connecting areas 9 have a width that increases in the circumferential direction of the oil control ring spring 1 towards the nose sections 13.
- the oil control ring spring 1 with the upper metal ring 21 or lower metal ring 23 placed on both sides is arranged as an oil control ring 3 running in a groove of a piston of an internal combustion engine.
- the oil control ring spring 1 is then reciprocated during operation in its axial direction relative to a cylinder in which the piston works.
- Excess oil that collects between the upper metal ring 21 and the lower metal ring 23 in the area of the oil control ring spring 1 can radially via the recesses 19 in the support sections 17 and the through openings 15 in the nose sections 13 be discharged.
- the depressions 19 and, in this exemplary embodiment, the through openings 15, which are aligned with the depressions 19, work together for good oil transport.
- Combustion and oil residues can thereby be effectively removed from the area of the oil control ring spring 1, ie the area between the upper metal ring 21 and the lower metal ring 23. This can reduce the friction in the engine, increase the efficiency of the engine, extend the service life of the engine and improve pollutant emissions.
- FIG. 8 shows the oil control ring spring 1 according to the exemplary embodiment from FIG Fig. 1 as an enlarged view at the point marked with the letter F in the left side view in Fig. 1 is marked.
- the outer circumference of the oil control ring spring 1 faces the viewer, while the inner circumferential end with the nose sections 13 lies at the bottom in the plane of the drawing.
- the nose sections 13 protrude to the left or to the right from the essentially vertical extent of the section of the oil control ring spring 1.
- the lower areas 7 with the nose sections provided there can now also be seen.
- the lower areas 7 protrude to the right in the picture, while the upper areas 5 run to the left.
- the depressions 19 cannot be seen directly in this view, but protuberances 25 can be seen which form the bottom of the depressions 19 and which are due to the shape of the depressions 19 and the realization as a sheet metal part.
- FIG. 8 shows the oil control ring spring 1 according to the exemplary embodiment from FIG Fig. 1 as an enlarged detail E of section AA, as on the right in Fig. 1 marked.
- the nose sections 13 are at the front of the picture.
- the viewer's gaze falls through the through opening 15 radially outward into the recess 19.
- the recess 19 in the upper area 5 shows itself as a protuberance radially in the direction of the lower areas 7 in the material of the oil control ring spring 1.
- the support sections 17 can be seen through the through openings 15 as essentially vertical lines.
- Fig. 5 shows an oil control ring 3 according to a first embodiment as a detail as in the lateral sectional view in FIG Fig. 4 .
- the oil control ring 3 has an oil control ring spring 1 which runs between an upper metal ring 21 and a lower metal ring 23.
- the metal rings 21, 23 are pressed apart or kept at a distance by the oil control ring spring 1.
- the oil control ring spring 1 is as in Figs. 1 to 4 described designed.
- the nose sections 13 are arranged to the rear into the image plane, which now grip behind the metal rings 21, 23 arranged in front of the image plane and delimit or press them radially outwards.
- Fig. 6 shows the oil control ring 3 according to the first embodiment as a sectional view.
- the upper metal ring 21 is shown as a rounded rectangle above the lower metal ring 23.
- the oil control ring spring 1 is arranged between the two metal rings 21, 23 and is shown partially hatched.
- a recess angle 27 indicates the angle which the top of the bottom of the recess 19 encloses with the radial plane of the oil control ring spring 1.
- the depth of the recess 19 increases from left to right up to its maximum depth, i.e. maximum distance from the upper metal ring 21 resting on the oil control ring spring 1.
- the spacing between the lower metal ring 23 and the upper metal ring 21 by the oil control ring spring 1 is dimensioned with a support height 29.
- An axial metal ring thickness 31 as its extension in the axial direction and a radial metal ring width 33 as its extension in the radial direction are shown as dimensions on the lower metal ring 23.
- a shoulder 35 can be seen on the oil control ring spring 1 according to this exemplary embodiment, which extends in the direction of the upper metal ring 21 and serves to rest the upper metal ring 21.
- a A corresponding shoulder 35 is provided on the oil control ring spring 1 for the lower metal ring 23 to rest on, but cannot be seen in this illustration.
- the shoulder has a shoulder height 37 with which it protrudes radially above the level of the beginning of the recess 19 in the direction of the upper metal ring 21.
- a shoulder length 39 of the shoulder 35 indicates its extension radially along the oil control ring spring 1. An increase in the shoulder length 39 accordingly causes an increase in the contact area between the respective metal ring 21, 23 and the associated shoulder 35.
- An axial spring height 41 of the oil control ring spring 1 denotes its extension, that is to say its dimension, in the axial direction.
- a radial spring width 43 of the oil control ring spring 1 indicates its extension in the radial direction of the oil control ring spring 1.
- a material thickness 45 is shown in the hatched area of the oil control ring spring 1 running perpendicularly into the plane of the paper.
- the oil control ring spring 1 is produced as a bent sheet metal part from a sheet metal corresponding to the material thickness 45.
- a thickness 47 of the nose section 13 is indicated in this figure.
- the thickness 47 corresponds to a radial extension of the nose section 13 starting at the end of the recess 19 to the radial end of the nose section 13.
- An angle 49 of the nose section 13 corresponds to its inclination relative to the axial direction of the oil control ring spring 1. The angle 49 causes an axial pressure apart of the metal rings 21, 23 resulting from a radial pressing force between the nose section 13 angled at the angle 49 and the metal rings 21, 23.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102017108683.8A DE102017108683A1 (de) | 2017-04-24 | 2017-04-24 | Ölabstreifring-Feder für einen Ölabstreifring und Ölabstreifring |
PCT/EP2018/060414 WO2018197450A1 (de) | 2017-04-24 | 2018-04-24 | Ölabstreifring-feder für einen ölabstreifring und ölabstreifring |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3615849A1 EP3615849A1 (de) | 2020-03-04 |
EP3615849B1 true EP3615849B1 (de) | 2021-12-08 |
Family
ID=62044745
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18719565.6A Active EP3615849B1 (de) | 2017-04-24 | 2018-04-24 | Ölabstreifring-feder für einen ölabstreifring und ölabstreifring |
Country Status (8)
Country | Link |
---|---|
US (1) | US11143301B2 (zh) |
EP (1) | EP3615849B1 (zh) |
CN (1) | CN110709628B (zh) |
BR (1) | BR112019022147B1 (zh) |
DE (1) | DE102017108683A1 (zh) |
ES (1) | ES2908684T3 (zh) |
PT (1) | PT3615849T (zh) |
WO (1) | WO2018197450A1 (zh) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2778481A1 (en) * | 2011-11-11 | 2014-09-17 | TPR Co., Ltd. | Combination oil ring |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2904377A (en) * | 1957-05-21 | 1959-09-15 | Muskegon Piston Ring Co Inc | Spacer and expander for piston rings |
US5195758A (en) * | 1991-11-19 | 1993-03-23 | Hastings Manufacturing Company | Three-piece oil control ring assembly |
JP5557562B2 (ja) * | 2010-03-10 | 2014-07-23 | Tpr株式会社 | 組合せオイルリング |
JP5970200B2 (ja) * | 2011-04-20 | 2016-08-17 | Tpr株式会社 | 組合せオイルリング |
JP5970239B2 (ja) * | 2012-05-28 | 2016-08-17 | 株式会社リケン | 組合せオイルコントロールリング |
JP6211332B2 (ja) * | 2012-07-27 | 2017-10-11 | 日本ピストンリング株式会社 | 組合せオイルリング |
JP2014209018A (ja) * | 2012-08-30 | 2014-11-06 | 日本ピストンリング株式会社 | 組合せオイルリング |
JP6543331B2 (ja) * | 2015-03-31 | 2019-07-10 | 日本ピストンリング株式会社 | 組合せオイルリング |
-
2017
- 2017-04-24 DE DE102017108683.8A patent/DE102017108683A1/de not_active Ceased
-
2018
- 2018-04-24 PT PT187195656T patent/PT3615849T/pt unknown
- 2018-04-24 CN CN201880026750.2A patent/CN110709628B/zh active Active
- 2018-04-24 ES ES18719565T patent/ES2908684T3/es active Active
- 2018-04-24 BR BR112019022147-6A patent/BR112019022147B1/pt active IP Right Grant
- 2018-04-24 EP EP18719565.6A patent/EP3615849B1/de active Active
- 2018-04-24 US US16/607,547 patent/US11143301B2/en active Active
- 2018-04-24 WO PCT/EP2018/060414 patent/WO2018197450A1/de unknown
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2778481A1 (en) * | 2011-11-11 | 2014-09-17 | TPR Co., Ltd. | Combination oil ring |
Also Published As
Publication number | Publication date |
---|---|
WO2018197450A1 (de) | 2018-11-01 |
CN110709628A (zh) | 2020-01-17 |
DE102017108683A1 (de) | 2018-10-25 |
EP3615849A1 (de) | 2020-03-04 |
PT3615849T (pt) | 2022-02-15 |
US20200072352A1 (en) | 2020-03-05 |
BR112019022147A2 (pt) | 2020-05-12 |
BR112019022147B1 (pt) | 2023-05-02 |
US11143301B2 (en) | 2021-10-12 |
CN110709628B (zh) | 2021-07-20 |
ES2908684T3 (es) | 2022-05-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1985898A1 (de) | Metallische Flachdichtung | |
WO2010063258A1 (de) | Kammkäfig für ein wälzlager, insbesondere ein doppelkammkäfig für ein zylinderrollenlager, wälzlager und verfahren zum herstellen eines kammkäfigs für ein wälzlager | |
EP1521929B2 (de) | Kolben für einen verbrennungsmotor | |
EP1156242B2 (de) | Radialwellendichtring | |
EP2162648B1 (de) | Kolbenring für den kolben eines verbrennungsmotors | |
DE3879825T2 (de) | Zylinderhaftdichtung mit einem brennraum-dichtelement, welches wie ein balken funktioniert. | |
DE102006056502B4 (de) | Käfig für ein Wälzlager und Verfahren zu seiner Herstellung | |
EP3615849B1 (de) | Ölabstreifring-feder für einen ölabstreifring und ölabstreifring | |
EP3797232B1 (de) | Mehrteiliger ölabstreif-kolbenring mit verringerter reibung | |
DE2720501C2 (de) | Ölabstreifring | |
AT521716B1 (de) | Ölabstreifring für eine Kolbenstange | |
EP0939256B1 (de) | Dichtungssystem | |
EP3492782B1 (de) | Ölabstreifring-feder für einen ölabstreifring und ölabstreifring | |
EP0789100A2 (de) | Gestanztes Strickwerkzeug | |
WO2004081424A1 (de) | Flachdichtung, insbesondere zylinderkopfdichtung | |
DE102019112614B3 (de) | Ölabstreifring mit einseitig angeordneten Rails | |
WO2006125416A1 (de) | Dichtpaket und hubkolben mit einem solchen paket | |
EP1377397A2 (de) | Werkzeug zum nietartigen verbinden | |
DE102005047452B4 (de) | Verstelleinrichtung für einen Fahrzeugsitz | |
EP0758281B1 (de) | Schneideinsatz, insbesondere zum fräsen | |
DE102017107009B4 (de) | Spielfreier Ölabstreifring | |
DE602004003943T2 (de) | Metalltreibriemen | |
EP3797233A1 (de) | Dreiteiliger ölabstreifring | |
DE10118910B4 (de) | Kolbenringanordnung | |
EP4136370B1 (de) | Ölabstreifring für kolben eines verbrennungsmotors |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: UNKNOWN |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20191105 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
17Q | First examination report despatched |
Effective date: 20201023 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: GRANT OF PATENT IS INTENDED |
|
INTG | Intention to grant announced |
Effective date: 20210628 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE PATENT HAS BEEN GRANTED |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 1454020 Country of ref document: AT Kind code of ref document: T Effective date: 20211215 Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502018008130 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: SC4A Ref document number: 3615849 Country of ref document: PT Date of ref document: 20220215 Kind code of ref document: T Free format text: AVAILABILITY OF NATIONAL TRANSLATION Effective date: 20220209 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG9D |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20211208 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220308 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2908684 Country of ref document: ES Kind code of ref document: T3 Effective date: 20220503 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220308 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220309 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502018008130 Country of ref document: DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20220408 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
26N | No opposition filed |
Effective date: 20220909 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20220424 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20220430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220424 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220430 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220424 Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220430 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220430 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20220424 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: PT Payment date: 20230422 Year of fee payment: 6 Ref country code: ES Payment date: 20230517 Year of fee payment: 6 Ref country code: DE Payment date: 20230626 Year of fee payment: 6 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Effective date: 20230807 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20211208 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20180424 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 1454020 Country of ref document: AT Kind code of ref document: T Effective date: 20230424 |